DocumentCode :
3328282
Title :
Velocity magnitude control of maneuverable reentry warhead
Author :
Kaifeng Liu ; Xinxue Liu ; Fang Wang ; Jian Wu
Author_Institution :
Xi´an Res. Inst. of High-tech, Xi´an, China
Volume :
1
fYear :
2011
fDate :
22-24 Aug. 2011
Firstpage :
374
Lastpage :
377
Abstract :
In this paper, the kinematic model of reentry warhead was built to verify the effect of control law. Then, an idea velocity curve was designed to support a standard of velocity control and the calculation of attack angle and sideslip angle was discussed. Finally, the efficiency of control law was verified through simulation. The simulation result shows that the control law proposed in this paper can limit the velocity magnitude error within 10m without losing accuracy of control of fall point and velocity direction.
Keywords :
military systems; velocity control; weapons; attack angle; kinematic model; maneuverable reentry warhead; reentry warhead; velocity control; velocity curve; velocity magnitude control; ideal velocity curve; reentry maneuverable warhead; supplementary attack angle; velocity magnitude control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Strategic Technology (IFOST), 2011 6th International Forum on
Conference_Location :
Harbin, Heilongjiang
Print_ISBN :
978-1-4577-0398-0
Type :
conf
DOI :
10.1109/IFOST.2011.6021043
Filename :
6021043
Link To Document :
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